Propulsion System Flow Stability Program (Dynamic). Part VIII. Model for Predicting Compressor Performance with Combined Circumferential and Radial Distortion - Computer Program.

Item

Title
Propulsion System Flow Stability Program (Dynamic). Part VIII. Model for Predicting Compressor Performance with Combined Circumferential and Radial Distortion - Computer Program.
Date
1968
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
AFAPL TR 68-142 Part VIII
Creator
Novak, R. A.
Hearsey, R. M.
Corporate Author
Northern Research and Engineering Corporation
Extent
304
NTRL Accession Number
AD851903
Identifier
AD0851903
AD0851903
Distribution Classification
1
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
AFAPL LTR
Abstract
The report describes in detail a computer program designed to enable the performance of axial flow compressors operating under asymmetric inlet conditions to be predicted. The underlying theory is given in Part VII; a comparison between results obtained and experimental data is made in Part IX. The report is divided into a number of sections, the principal ones being those giving a Functional Discription of the program, and an Operational Description of the program. The Functional Description is intended to enable the program to be used. The Operational Description of the program is intended to enable the methods used in the program to be understood in detail, hence allowing the program to be modified if desired.
Report Availability
Full text available
Date Issued
1968-12
Laboratory
Air Force Aero Propulsion Laboratory
Contract
F333615-67-C-1848
Distribution Conflict
No
Access Rights
Export Controls
Date Modified
Scanned by request 1/9/2019 submitted by Illinois Institute of Technology (University - Domestic)
Publisher
Wright-Patterson Air Force Base, OH : Air Force Aero Propulsion Laboratory, Air Force Systems Command
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Media
AFAPLTR68-142part08.pdf